TY - JOUR
T1 - Reachability calculations for vehicle safety during manned/unmanned vehicle interaction
AU - Ding, Jerry
AU - Sprinkle, Jonathan
AU - Tomlin, Claire J.
AU - Sastry, S. Shankar
AU - Paunicka, James L.
N1 - Funding Information:
This work was supported in part by the Certification Technologies for Flight Critical Systems project, U.S. Air Force Research Laboratory (AFRL), through a contract with Boeing Research &; Technology, and in part by the Center for Hybrid and Embedded Software Systems at the University of California, Berkeley, which receives support from the National Science Foundation (NSF, awards CCR-0225610, 0720882, 0647591, and 0720841, the U. S. Army Research Office (W911NF-07-2-0019), U.S. Air Force Office of Scientific Research (AFOSR) awards FA9550-06-0312 and FA9550-06-1-0244, AFRL, the State of California Micro Program, and the following companies: Agilent, Bosch, DGIST, Lockheed Martin, National Instruments, and Toyota. Additional support was provided by AFOSR award FA9550-091-0519, titled “Modeling of Embedded Human Systems,” and NSF awards CNS-0915010 and CNS-0930919. The authors gratefully acknowledge the additional contributions of Doug Stuart and Jim Barhorst of Boeing Research & Technology, who aided in the development of the automated aerial refueling scenario and provided valuable feedback with regard to questions of discrete reachability. Also, many of the research ideas that produced this work were conceived in David Homan’s yearly meetings on verification and validation at Wright-Patterson Air Force Base. In those meetings, this work was influenced in the conversation and presentations of many of those participants, and the authors are grateful for their contribution.
PY - 2012
Y1 - 2012
N2 - This paper describes an approach based on reachability calculations for ensuring robust operation guarantees in flight maneuver sequences performed by unmanned aerial vehicles under supervision of human operators, with applications to safety-critical scenarios. Using a hybrid system formalism to model the maneuver sequence, the paper devises systematic procedures for designing switching conditions to ensure the properties of safety, target attainability, and invariance, using Hamilton-Jacobi reachability calculations. These calculations lay the foundations for refining or designing protocols for multiple unmanned aerial vehicle and/or manned vehicle interaction. The mathematical foundations necessary are described in order to formulate verification problems on reachability and safety of flight maneuvers, including issues of command latency and disturbance. An example of this formalism is given in the context of automated aerial refueling, to inform unmanned aerial vehicle decisions that avoid unsafe scenarios while achieving mission objectives.
AB - This paper describes an approach based on reachability calculations for ensuring robust operation guarantees in flight maneuver sequences performed by unmanned aerial vehicles under supervision of human operators, with applications to safety-critical scenarios. Using a hybrid system formalism to model the maneuver sequence, the paper devises systematic procedures for designing switching conditions to ensure the properties of safety, target attainability, and invariance, using Hamilton-Jacobi reachability calculations. These calculations lay the foundations for refining or designing protocols for multiple unmanned aerial vehicle and/or manned vehicle interaction. The mathematical foundations necessary are described in order to formulate verification problems on reachability and safety of flight maneuvers, including issues of command latency and disturbance. An example of this formalism is given in the context of automated aerial refueling, to inform unmanned aerial vehicle decisions that avoid unsafe scenarios while achieving mission objectives.
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U2 - 10.2514/1.53706
DO - 10.2514/1.53706
M3 - Article
AN - SCOPUS:84855319399
SN - 0731-5090
VL - 35
SP - 138
EP - 152
JO - Journal of Guidance, Control, and Dynamics
JF - Journal of Guidance, Control, and Dynamics
IS - 1
ER -